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1680-01-394-6291

Aircraft Seat Frame

1680013946291 013946291 103021-1

A rigid metallic item designed to provide the basic structure of a SEAT (1), AIRCRAFT or SEAT (1), AIRCRAFT EJECTION. View more Aircraft Seat Frame

1680-01-394-6291 FRAME,SEAT,AIRCRAFT 1680013946291 013946291

Managed by United States
NSN Created on 12 Aug 1994
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
1680-01-394-6291 FRAME,SEAT,AIRCRAFT 1680013946291 013946291 1/1
NSN 1680-01-394-6291 (Generic Image) 1/1

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(CAGE Code 54786) Aug 1994 1680-01-394-6291 Aircraft Seat Frame 103021-1RNCC: 3 | RNVC: 2 | DAC: A 12
2010 1680-01-543-3334 Aircraft Seat Frame AL1040-55-00RNCC: 3 | RNVC: 2 | DAC: 6 8 Sep 2006 1680-01-394-6291

1680-01-394-6291 Demil Restrictions 1680-01-394-6291

DEMIL: A | DEMILI: 7 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

1680-01-394-6291 is a Aircraft Seat Frame that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

1680-01-394-6291 HTS and ScheduleB Import and Export 1680-01-394-6291

1680-01-394-6291 End Users End Users 1680-01-394-6291

US Air Force (FBB5)
Effective Date:
1 Oct 2000
Former MOE Rule:
FXCX

1680-01-394-6291 Manufacturers Approved Sources 1680-01-394-6291

1680-01-394-6291 Technical Data Datasheet 1680-01-394-6291

Characteristic
Specifications
FIIG
A11800
Material [MATT]
Aluminum Alloy
Aircraft Location [CZDJ]
Seat Sidewall
Aircraft Mission Design Series [CZEK]
C-17
Special Features [FEAT]
Seat Pan Assy
End Item Identification [AGAV]
C-17 Globmaster Aircraft

1680-01-394-6291 Management Data Management Data 1680-01-394-6291

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Aug 2005
Department of the Air Force (DF)
EA
Subscribe

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
Price Validation Code:
N
The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of ā€œLā€ or ā€œFā€, then it must be evaluated locally where purchased or fabricated.
Expendability
Recoverability
Repairability:
P
Expendable. Reparable. Condemn at Intermediate. Stock Fund (except Munitions).

1680-01-394-6291 Related Items NATO Stock Numbers Related to 1680-01-394-6291

1680-01-394-6291 Freight Data Freight Information 1680-01-394-6291

1680-01-394-6291 has freight characteristics.. 1680-01-394-6291 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

1680-01-394-6291 Packaging Data Packaging Data 1680-01-394-6291

Responsible Activity
Packaging Data Source
Primary Inventory Control Activity (PICA)
Packaging Data does not meet current MIL-STD-2073-1E

Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation
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--
--
--
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Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
--
--
--
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Physical Protection
Any Suitable Process
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
No Requirement
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--
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PPP-B-566, PPP-B-676, or ASTM-D5118, Folding, Setup or Fiberboard Box
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Intermediate Pack Level

Quantity of Unit Packs
Container
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